Research on Design and Analysis Platform for Modular Spacecraft

Xiao-wen Zeng (), Zhao-xia He () and Hao Luo
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Xiao-wen Zeng: Hunan Institute of Science and Technology
Zhao-xia He: Chang’an University
Hao Luo: Northwestern Polytechnical University

Chapter Chapter 133 in The 19th International Conference on Industrial Engineering and Engineering Management, 2013, pp 1263-1272 from Springer

Abstract: Abstract In spacecraft structure design process, modular technology is very important for improving efficiency and reducing cost. Based on the modular design method, a deployable on-orbit spacecraft modular configuration was established. The influence of simultaneously deployment solar panel and modular structures under the situation of weightlessness on the spacecraft’s gesture was simulated and analyzed with the assistance of virtual prototype technology. The simulated result shows that the deployment of module structures is vital to the angle of spacecraft’s gesture and its velocity. Within the Eclipse development environment, an integrated platform which includes design and analysis for spacecraft was developed with J2EE. In order to acquire rapid response to the whole process, which includes structural design, digital prototype assembly and dynamics analysis, the structure design, assembly and dynamics analysis of spacecraft were well integrated.

Keywords: Integrated platform; Modular design; Spacecraft; Virtual prototype technology (search for similar items in EconPapers)
Date: 2013
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Persistent link: https://EconPapers.repec.org/RePEc:spr:sprchp:978-3-642-38391-5_133

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DOI: 10.1007/978-3-642-38391-5_133

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